Uses of Interface
org.orekit.attitudes.AttitudeProvider

Packages that use AttitudeProvider

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.estimation.measurements.modifiers	This package provides measurement modifier.
org.orekit.forces.empirical	This package provides empirical forces.
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.forces.maneuvers.propulsion	This package provides propulsion models intended to be used with class Maneuver.
org.orekit.gnss.attitude	This package provides classes related to navigation satellites attitude modeling.
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.propagation	Propagation
org.orekit.propagation.analytical	Top level package for analytical propagators.
org.orekit.propagation.analytical.gnss	This package provides classes to propagate GNSS orbits.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.forces	This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.utils	This package provides useful objects.

Uses of AttitudeProvider in org.orekit.attitudes

Subinterfaces of AttitudeProvider in org.orekit.attitudes

Modifier and Type	Interface and Description
interface	AttitudeProviderModifier This interface represents an attitude provider that modifies/wraps another underlying provider.
interface	BoundedAttitudeProvider This interface is intended for attitude ephemerides valid only during a time range.

Classes in org.orekit.attitudes that implement AttitudeProvider

Modifier and Type	Class and Description
class	AggregateBoundedAttitudeProvider A BoundedAttitudeProvider that covers a larger time span from several constituent attitude providers that cover shorter time spans.
class	AttitudesSequence This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
class	BodyCenterPointing This class handles body center pointing attitude provider.
class	CelestialBodyPointed This class handles a celestial body pointed attitude provider.
class	FixedRate This class handles a simple attitude provider at constant rate around a fixed axis.
class	GroundPointing Base class for ground pointing attitude providers.
class	InertialProvider This class handles an attitude provider aligned with a frame or a fixed offset to it.
class	LofOffset Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.
class	LofOffsetPointing This class provides a default attitude provider.
class	NadirPointing This class handles nadir pointing attitude provider.
class	SpinStabilized This class handles a spin stabilized attitude provider.
class	TabulatedLofOffset This class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.
class	TabulatedProvider This class handles an attitude provider interpolating from a predefined table.
class	TargetPointing This class handles target pointing attitude provider.
class	YawCompensation This class handles yaw compensation attitude provider.
class	YawSteering This class handles yaw steering law.

Methods in org.orekit.attitudes that return AttitudeProvider

Modifier and Type	Method and Description
AttitudeProvider	YawCompensation.getUnderlyingAttitudeProvider() Get the underlying (ground pointing) attitude provider.
AttitudeProvider	AttitudeProviderModifier.getUnderlyingAttitudeProvider() Get the underlying attitude provider.
AttitudeProvider	SpinStabilized.getUnderlyingAttitudeProvider() Get the underlying attitude provider.
AttitudeProvider	YawSteering.getUnderlyingAttitudeProvider() Get the underlying (ground pointing) attitude provider.
static AttitudeProvider	InertialProvider.of(Frame satelliteFrame) Creates an attitude provider aligned with the given frame.

Methods in org.orekit.attitudes with parameters of type AttitudeProvider

Modifier and Type	Method and Description
<T extends EventDetector> void	AttitudesSequence.addSwitchingCondition(AttitudeProvider past, AttitudeProvider future, T switchEvent, boolean switchOnIncrease, boolean switchOnDecrease, double transitionTime, AngularDerivativesFilter transitionFilter, AttitudesSequence.SwitchHandler handler) Add a switching condition between two attitude providers.
void	AttitudesSequence.resetActiveProvider(AttitudeProvider provider) Reset the active provider.
void	AttitudesSequence.SwitchHandler.switchOccurred(AttitudeProvider preceding, AttitudeProvider following, SpacecraftState state) Method called when attitude is switched from one law to another law.

Constructors in org.orekit.attitudes with parameters of type AttitudeProvider

Constructor and Description
LofOffsetPointing(Frame inertialFrame, BodyShape shape, AttitudeProvider attLaw, Vector3D satPointingVector) Creates new instance.
SpinStabilized(AttitudeProvider nonRotatingLaw, AbsoluteDate start, Vector3D axis, double rate) Creates a new instance.

Uses of AttitudeProvider in org.orekit.estimation.measurements.modifiers

Constructors in org.orekit.estimation.measurements.modifiers with parameters of type AttitudeProvider

Constructor and Description
IonosphericGradientConverter(SpacecraftState state, int freeStateParameters, AttitudeProvider provider) Deprecated. Simple constructor.
ModifierGradientConverter(SpacecraftState state, int freeStateParameters, AttitudeProvider provider) Simple constructor.
OnBoardAntennaOneWayGNSSPhaseModifier(Vector3D antennaPhaseCenter1, Vector3D antennaPhaseCenter2, AttitudeProvider attitude) Simple constructor.
OnBoardAntennaOneWayGNSSRangeModifier(Vector3D antennaPhaseCenter1, Vector3D antennaPhaseCenter2, AttitudeProvider attitude) Simple constructor.
TroposphericGradientConverter(SpacecraftState state, int freeStateParameters, AttitudeProvider provider) Deprecated. Simple constructor.

Uses of AttitudeProvider in org.orekit.forces.empirical

Constructors in org.orekit.forces.empirical with parameters of type AttitudeProvider

Constructor and Description
ParametricAcceleration(Vector3D direction, AttitudeProvider attitudeOverride, AccelerationModel accelerationModel) Simple constructor.
TimeSpanParametricAcceleration(Vector3D direction, AttitudeProvider attitudeOverride, AccelerationModel accelerationModel) Simple constructor.

Uses of AttitudeProvider in org.orekit.forces.maneuvers

Methods in org.orekit.forces.maneuvers that return AttitudeProvider

Modifier and Type	Method and Description
AttitudeProvider	Maneuver.getAttitudeOverride() Get the attitude override used for the maneuver.
AttitudeProvider	ImpulseManeuver.getAttitudeOverride() Get the Attitude Provider to use during maneuver.

Constructors in org.orekit.forces.maneuvers with parameters of type AttitudeProvider

Constructor and Description
ConstantThrustManeuver(AbsoluteDate date, double duration, AttitudeProvider attitudeOverride, AbstractConstantThrustPropulsionModel constantThrustPropulsionModel) Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate date, double duration, double thrust, double isp, AttitudeProvider attitudeOverride, Vector3D direction) Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate date, double duration, double thrust, double isp, AttitudeProvider attitudeOverride, Vector3D direction, String name) Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AttitudeProvider attitudeOverride, DateBasedManeuverTriggers dateBasedManeuverTriggers, AbstractConstantThrustPropulsionModel constantThrustPropulsionModel) Simple constructor for a constant direction and constant thrust.
ImpulseManeuver(T trigger, AttitudeProvider attitudeOverride, Vector3D deltaVSat, double isp) Build a new instance.
Maneuver(AttitudeProvider attitudeOverride, ManeuverTriggers maneuverTriggers, PropulsionModel propulsionModel) Generic maneuver constructor.

Uses of AttitudeProvider in org.orekit.forces.maneuvers.propulsion

Classes in org.orekit.forces.maneuvers.propulsion that implement AttitudeProvider

Modifier and Type	Class and Description
class	ThrustDirectionAndAttitudeProvider This class is used in to both manage the attitude of the satellite and the direction of thrust.

Methods in org.orekit.forces.maneuvers.propulsion that return AttitudeProvider

Modifier and Type	Method and Description
AttitudeProvider	ThrustDirectionAndAttitudeProvider.getManeuverAttitudeProvider() Attitude provider to use.

Methods in org.orekit.forces.maneuvers.propulsion with parameters of type AttitudeProvider

Modifier and Type	Method and Description
static ThrustDirectionAndAttitudeProvider	ThrustDirectionAndAttitudeProvider.buildFromCustomAttitude(AttitudeProvider attitudeProvider, Vector3D direction) Build a ThrustDirectionAndAttitudeProvider where the attitude is provided by an external.

Uses of AttitudeProvider in org.orekit.gnss.attitude

Subinterfaces of AttitudeProvider in org.orekit.gnss.attitude

Modifier and Type	Interface and Description
interface	GNSSAttitudeProvider Attitude providers for navigation satellites.

Classes in org.orekit.gnss.attitude that implement AttitudeProvider

Modifier and Type	Class and Description
class	BeidouGeo Attitude providers for Beidou geostationary orbit navigation satellites.
class	BeidouIGSO Attitude providers for Beidou inclined geosynchronous orbit navigation satellites.
class	BeidouMeo Attitude providers for Beidou Medium Earth Orbit navigation satellites.
class	Galileo Attitude providers for Galileo navigation satellites.
class	GenericGNSS Attitude providers for navigation satellites for which no specialized model is known.
class	Glonass Attitude providers for Glonass navigation satellites.
class	GPSBlockIIA Attitude providers for GPS block IIA navigation satellites.
class	GPSBlockIIF Attitude providers for GPS block IIF navigation satellites.
class	GPSBlockIIR Attitude providers for GPS block IIR navigation satellites.

Uses of AttitudeProvider in org.orekit.orbits

Methods in org.orekit.orbits with parameters of type AttitudeProvider

Modifier and Type	Method and Description
void	LibrationOrbit.applyDifferentialCorrection(AttitudeProvider attitudeProvider, TimeScale utc) Deprecated. as of 11.1, replaced by LibrationOrbit.applyDifferentialCorrection()

Constructors in org.orekit.orbits with parameters of type AttitudeProvider

Constructor and Description
CR3BPDifferentialCorrection(PVCoordinates firstguess, CR3BPSystem syst, double orbitalPeriod, AttitudeProvider attitudeProvider, TimeScale utc) Deprecated. as of 11.1, replaced by CR3BPDifferentialCorrection.CR3BPDifferentialCorrection(PVCoordinates, CR3BPSystem, double)

Uses of AttitudeProvider in org.orekit.propagation

Methods in org.orekit.propagation that return AttitudeProvider

Modifier and Type	Method and Description
AttitudeProvider	Propagator.getAttitudeProvider() Get attitude provider.
AttitudeProvider	FieldPropagator.getAttitudeProvider() Get attitude provider.
AttitudeProvider	AbstractPropagator.getAttitudeProvider() Get attitude provider.
AttitudeProvider	FieldAbstractPropagator.getAttitudeProvider() Get attitude provider.
static AttitudeProvider	Propagator.getDefaultLaw(Frames frames) Get a default law using the given frames.

Methods in org.orekit.propagation with parameters of type AttitudeProvider

Modifier and Type	Method and Description
void	Propagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider.
void	FieldPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider.
void	AbstractPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider.
void	FieldAbstractPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider.

Uses of AttitudeProvider in org.orekit.propagation.analytical

Constructors in org.orekit.propagation.analytical with parameters of type AttitudeProvider

Constructor and Description
AbstractAnalyticalPropagator(AttitudeProvider attitudeProvider) Build a new instance.
BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double M2) Build a propagator from orbit, attitude provider and potential.
BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double M2) Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, PropagationType initialType, double M2) Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, PropagationType initialType, double M2, double epsilon, int maxIterations) Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, UnnormalizedSphericalHarmonicsProvider provider, double M2) Build a propagator from orbit, attitude provider, mass and potential provider.
BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType, double M2) Build a propagator from orbit, attitude provider, mass and potential provider.
BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitude, double mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double M2) Private helper constructor.
BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitude, double mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType, double M2) Private helper constructor.
BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider, double M2) Build a propagator from orbit, attitude provider and potential provider.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60) Build a propagator from orbit, attitude provider and potential.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60) Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType) Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType, double epsilon, int maxIterations) Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, UnnormalizedSphericalHarmonicsProvider provider) Build a propagator from orbit, attitude provider, mass and potential provider.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType) Build a propagator from orbit, attitude provider, mass and potential provider.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitude, double mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics) Private helper constructor.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitude, double mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType) Private helper constructor.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider) Build a propagator from orbit, attitude provider and potential provider.
Ephemeris(List<SpacecraftState> states, int interpolationPoints, double extrapolationThreshold, AttitudeProvider attitudeProvider) Constructor with tabulated states.
FieldAbstractAnalyticalPropagator(Field<T> field, AttitudeProvider attitudeProvider) Build a new instance.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double M2) Build a propagator from orbit, attitude provider and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double M2) Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, PropagationType initialType, double M2) Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, PropagationType initialType, double M2, double epsilon, int maxIterations) Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, double M2) Build a propagator from orbit, attitude provider, mass and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType, double M2) Build a propagator from orbit, attitude provider, mass and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double M2) Private helper constructor.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType, double M2) Private helper constructor.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider, double M2) Build a propagator from orbit, attitude provider and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60) Build a propagator from FieldOrbit, attitude provider and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60) Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType) Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType, double epsilon, int maxIterations) Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider) Build a propagator from FieldOrbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType) Build a propagator from orbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics) Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType) Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider) Build a propagator from FieldOrbit, attitude provider and potential provider.
FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, AttitudeProvider attitudeProv) Build a propagator from orbit and attitude provider.
FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, AttitudeProvider attitudeProv, T mu) Build a propagator from orbit, attitude provider and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mu, T mass) Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv) Build a propagator from orbit and attitude provider.
KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mu) Build a propagator from orbit, attitude provider and central attraction coefficient μ.
KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mu, double mass) Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.

Uses of AttitudeProvider in org.orekit.propagation.analytical.gnss

Methods in org.orekit.propagation.analytical.gnss with parameters of type AttitudeProvider

Modifier and Type	Method and Description
GNSSPropagatorBuilder	GNSSPropagatorBuilder.attitudeProvider(AttitudeProvider userProvider) Sets the attitude provider.
GLONASSAnalyticalPropagatorBuilder	GLONASSAnalyticalPropagatorBuilder.attitudeProvider(AttitudeProvider userProvider) Sets the attitude provider.
SBASPropagatorBuilder	SBASPropagatorBuilder.attitudeProvider(AttitudeProvider userProvider) Sets the attitude provider.

Uses of AttitudeProvider in org.orekit.propagation.analytical.tle

Methods in org.orekit.propagation.analytical.tle with parameters of type AttitudeProvider

Modifier and Type	Method and Description
static <T extends CalculusFieldElement<T>> FieldTLEPropagator<T>	FieldTLEPropagator.selectExtrapolator(FieldTLE<T> tle, AttitudeProvider attitudeProvider, T mass, Frame teme, T[] parameters) Selects the extrapolator to use with the selected TLE.
static <T extends CalculusFieldElement<T>> FieldTLEPropagator<T>	FieldTLEPropagator.selectExtrapolator(FieldTLE<T> tle, AttitudeProvider attitudeProvider, T mass, T[] parameters) Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, double mass) Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, double mass, Frame teme) Selects the extrapolator to use with the selected TLE.

Constructors in org.orekit.propagation.analytical.tle with parameters of type AttitudeProvider

Constructor and Description
DeepSDP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass) Constructor for a unique initial TLE.
DeepSDP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass, Frame teme) Constructor for a unique initial TLE.
FieldDeepSDP4(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, Frame teme, T[] parameters) Constructor for a unique initial TLE.
FieldDeepSDP4(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, T[] parameters) Constructor for a unique initial TLE.
FieldSGP4(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, Frame teme, T[] parameters) Constructor for a unique initial TLE.
FieldSGP4(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, T[] parameters) Constructor for a unique initial TLE.
FieldTLEPropagator(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, Frame teme, T[] parameters) Protected constructor for derived classes.
FieldTLEPropagator(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, T[] parameters) Protected constructor for derived classes.
SGP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass) Constructor for a unique initial TLE.
SGP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass, Frame teme) Constructor for a unique initial TLE.
TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, double mass) Protected constructor for derived classes.
TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, double mass, Frame teme) Protected constructor for derived classes.

Uses of AttitudeProvider in org.orekit.propagation.conversion

Methods in org.orekit.propagation.conversion that return AttitudeProvider

Modifier and Type	Method and Description
AttitudeProvider	AbstractPropagatorBuilder.getAttitudeProvider() Get the attitude provider.

Methods in org.orekit.propagation.conversion with parameters of type AttitudeProvider

Modifier and Type	Method and Description
void	AbstractPropagatorBuilder.setAttitudeProvider(AttitudeProvider attitudeProvider) Set the attitude provider.

Constructors in org.orekit.propagation.conversion with parameters of type AttitudeProvider

Constructor and Description
AbstractPropagatorBuilder(Orbit templateOrbit, PositionAngle positionAngle, double positionScale, boolean addDriverForCentralAttraction, AttitudeProvider attitudeProvider) Build a new instance.
BrouwerLyddanePropagatorBuilder(Orbit templateOrbit, UnnormalizedSphericalHarmonicsProvider provider, PositionAngle positionAngle, double positionScale, AttitudeProvider attitudeProvider, double M2) Build a new instance.
DSSTPropagatorBuilder(Orbit referenceOrbit, ODEIntegratorBuilder builder, double positionScale, PropagationType propagationType, PropagationType stateType, AttitudeProvider attitudeProvider) Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit templateOrbit, UnnormalizedSphericalHarmonicsProvider provider, PositionAngle positionAngle, double positionScale, AttitudeProvider attitudeProvider) Build a new instance.
EphemerisPropagatorBuilder(List<SpacecraftState> states, int interpolationPoints, double extrapolationThreshold, AttitudeProvider attitudeProvider) Constructor.
KeplerianPropagatorBuilder(Orbit templateOrbit, PositionAngle positionAngle, double positionScale, AttitudeProvider attitudeProvider) Build a new instance.
NumericalPropagatorBuilder(Orbit referenceOrbit, ODEIntegratorBuilder builder, PositionAngle positionAngle, double positionScale, AttitudeProvider attitudeProvider) Build a new instance.

Uses of AttitudeProvider in org.orekit.propagation.integration

Methods in org.orekit.propagation.integration that return AttitudeProvider

Modifier and Type	Method and Description
AttitudeProvider	StateMapper.getAttitudeProvider() Get the attitude provider.
AttitudeProvider	FieldStateMapper.getAttitudeProvider() Get the attitude provider.

Methods in org.orekit.propagation.integration with parameters of type AttitudeProvider

Modifier and Type	Method and Description
protected abstract StateMapper	AbstractIntegratedPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.
protected abstract FieldStateMapper<T>	FieldAbstractIntegratedPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.
void	AbstractIntegratedPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider.
void	IntegratedEphemeris.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider.
void	StateMapper.setAttitudeProvider(AttitudeProvider attitudeProvider) Set the attitude provider.
void	FieldAbstractIntegratedPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider.

Constructors in org.orekit.propagation.integration with parameters of type AttitudeProvider

Constructor and Description
FieldStateMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Simple constructor.
StateMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Simple constructor.

Uses of AttitudeProvider in org.orekit.propagation.numerical

Methods in org.orekit.propagation.numerical with parameters of type AttitudeProvider

Modifier and Type	Method and Description
GLONASSNumericalPropagatorBuilder	GLONASSNumericalPropagatorBuilder.attitudeProvider(AttitudeProvider userProvider) Sets the attitude provider.
protected StateMapper	NumericalPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.
protected StateMapper	GLONASSNumericalPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame)
protected FieldStateMapper<T>	FieldNumericalPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.

Constructors in org.orekit.propagation.numerical with parameters of type AttitudeProvider

Constructor and Description
FieldNumericalPropagator(Field<T> field, FieldODEIntegrator<T> integrator, AttitudeProvider attitudeProvider) Create a new instance of NumericalPropagator, based on orbit definition mu.
GLONASSNumericalPropagator(ClassicalRungeKuttaIntegrator integrator, GLONASSOrbitalElements glonassOrbit, Frame eci, AttitudeProvider provider, double mass, DataContext context, boolean isAccAvailable) Private constructor.
NumericalPropagator(ODEIntegrator integrator, AttitudeProvider attitudeProvider) Create a new instance of NumericalPropagator, based on orbit definition mu.

Uses of AttitudeProvider in org.orekit.propagation.semianalytical.dsst

Methods in org.orekit.propagation.semianalytical.dsst with parameters of type AttitudeProvider

Modifier and Type	Method and Description
static <T extends CalculusFieldElement<T>> FieldSpacecraftState<T>	FieldDSSTPropagator.computeMeanState(FieldSpacecraftState<T> osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModel) Conversion from osculating to mean orbit.
static <T extends CalculusFieldElement<T>> FieldSpacecraftState<T>	FieldDSSTPropagator.computeMeanState(FieldSpacecraftState<T> osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModel, double epsilon, int maxIterations) Conversion from osculating to mean orbit.
static SpacecraftState	DSSTPropagator.computeMeanState(SpacecraftState osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModels) Conversion from osculating to mean orbit.
static SpacecraftState	DSSTPropagator.computeMeanState(SpacecraftState osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModels, double epsilon, int maxIterations) Conversion from osculating to mean orbit.
static <T extends CalculusFieldElement<T>> FieldSpacecraftState<T>	FieldDSSTPropagator.computeOsculatingState(FieldSpacecraftState<T> mean, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forces) Conversion from mean to osculating orbit.
static SpacecraftState	DSSTPropagator.computeOsculatingState(SpacecraftState mean, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forces) Conversion from mean to osculating orbit.
protected StateMapper	DSSTPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType ignoredOrbitType, PositionAngle ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.
protected FieldStateMapper<T>	FieldDSSTPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType ignoredOrbitType, PositionAngle ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.
void	FieldDSSTPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider.
void	DSSTPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider.

Constructors in org.orekit.propagation.semianalytical.dsst with parameters of type AttitudeProvider

Constructor and Description
DSSTPropagator(ODEIntegrator integrator, PropagationType propagationType, AttitudeProvider attitudeProvider) Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T> field, FieldODEIntegrator<T> integrator, AttitudeProvider attitudeProvider) Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T> field, FieldODEIntegrator<T> integrator, PropagationType propagationType, AttitudeProvider attitudeProvider) Create a new instance of DSSTPropagator.

Uses of AttitudeProvider in org.orekit.propagation.semianalytical.dsst.forces

Methods in org.orekit.propagation.semianalytical.dsst.forces with parameters of type AttitudeProvider

Modifier and Type	Method and Description
void	DSSTZonal.registerAttitudeProvider(AttitudeProvider attitudeProvider) Register an attitude provider.
void	AbstractGaussianContribution.registerAttitudeProvider(AttitudeProvider provider) Register an attitude provider.
void	DSSTNewtonianAttraction.registerAttitudeProvider(AttitudeProvider provider) Register an attitude provider.
void	DSSTForceModel.registerAttitudeProvider(AttitudeProvider provider) Register an attitude provider.
void	DSSTTesseral.registerAttitudeProvider(AttitudeProvider attitudeProvider) Register an attitude provider.
void	DSSTThirdBody.registerAttitudeProvider(AttitudeProvider provider) Register an attitude provider.

Uses of AttitudeProvider in org.orekit.utils

Methods in org.orekit.utils with parameters of type AttitudeProvider

Modifier and Type	Method and Description
static StateJacobian	Differentiation.differentiate(StateFunction function, int dimension, AttitudeProvider provider, OrbitType orbitType, PositionAngle positionAngle, double dP, int nbPoints) Differentiate a vector function using finite differences.